Performance on Contaminated Runways

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    Performance oncontaminated runways

    -Friction Coefficient - Crosswind - Use of FCOM

    Operations Liaison Meeting

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    2Performance on contaminated runways - Friction coefficient - Crosswind - Use of FCOM

    Content

    Runway condition: Airport information Correlation airport information/FCOM data

    FCOM data

    Performance determination

    Crosswind

    Conclusion

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    3Performance on contaminated runways - Friction coefficient - Crosswind - Use of FCOM

    A SNOWTAM contains :

    The type of contaminants,

    Mean depth for each third of the runway length,

    Estimated braking action,

    Reported Mu ()(Friction coefficient)

    Reported Mu Estimated

    Braking Action

    0.4 and above GOOD

    0.39 to 0.36MEDIUM/GOOD

    0.35 to 0.30 MEDIUM

    0.29 to 0.26

    MEDIUM/POOR

    0.25 and below POOR

    Runway condition: Airport information

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    4Performance on contaminated runways - Friction coefficient - Crosswind - Use of FCOM

    Airbus charts are provided by type of contaminants

    and the depth of contaminant on the runway.1/4 and 1/2 inch of slush, 1/4 and 1/2 inch of water, compacted snow

    A linear relation has been established between loose snow and slush,

    Sometimes, only the Estimated braking action orReported Mu is available.

    Is it possible to get the performance from a given reported Mu?

    Runway condition: Airport information

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    5Performance on contaminated runways - Friction coefficient - Crosswind - Use of FCOM

    Airports release a friction coefficient derived from

    a measuring vehicle. This friction coefficient is

    termed as reported Mu

    The actual friction coefficient, termed as effectiveMu (or aircraft Mu) is the result of the interaction

    tire/runway.

    It depends on the tire pressure, tire wear, aircraftspeed, aircraft weight and anti-skid system efficiency.

    Correlation airport information/FCOM dataEffective mu and reported mu

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    Measuring vehicles operate at much smaller weight

    and speed than aircraft.

    Tests have demonstrated that there is a poor

    correlationbetween the reported Mu and theeffective Mu. There is even a poor correlation in

    between the measuring vehicles.

    Even with an ideal reported Mu equals to the

    Effective Mu the type and depth of contaminants

    would be necessary.

    Correlation airport information/FCOM dataEffective mu and reported mu

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    There is a clearseparation in the effect of contaminants on

    the aircraft performance in hard and fluid contaminants

    Hard contaminants are : Compacted snow and ice

    Fluid contaminants are : Water, slush and loose snow.

    Hard: Decrease of friction forces

    Fluid: Decrease of friction forces +

    precipitation drag and aquaplaning

    Correlation airport information/FCOM dataHard and fluid contaminants

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    Precipitation drag The precipitation drag is composed of : Displacement drag

    produced by the displacement of the contaminant fluid from the path of

    the tire.

    Spray impingement drag

    produced by the spray thrown up by the wheels (mainly those of thenose gear) onto the fuselage.

    The effect of these additional drags must be

    accounted for:

    They affect the deceleration performance: positive effect.

    They affect the acceleration performance: negative effect.

    The effect on the acceleration leads to a limitation

    in the depth of fluid contaminants on the runway.

    Correlation airport information/FCOM data

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    Aquaplaning The presence of a fluid contaminant on the runway creates

    an intervening film between the tire and the runway

    leading to a reduction of the dry contact area.

    It gets more critical at higher speeds where the fluid

    cannot be squeezed out from between the tire and therunway.

    Aquaplaning is a situation where the tire of the aircraft are

    to a large extend separated from the runway surface.

    Friction forces drop to almost negligible values.

    Directional control and braking are virtually

    ineffective.

    Correlation airport information/FCOM data

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    Airbus does not provide the take-off and landingperformance on contaminated runways according to

    the reported braking action or to a reported .

    Aircraft performance on a fluid contaminated runway

    depends on the effective and the depth of fluid onthe runway.

    Charts are provided for: 1/4 inch water, 1/2 inch water, 1/4 inch slush, 1/2 inch slush.

    Aircraft performance on a hard contaminated runwaydepends on the effective .Charts are provided for: compacted snow (=0.2) and icy runway (=0.05)

    Correlation airport information/FCOM dataSummary

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    FCOM data

    Runway Conditions:

    Dry / Damp

    Wet

    Contaminated

    Different Contaminants:

    Standing Water

    Slush

    Wet Snow

    Dry Snow

    Compacted Snow

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    FCOM data

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    FCOM data

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    FCOM data

    Standing water:

    3 mm: wet

    > 3 mm: contaminated

    Different Contaminants - Standing Water

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    FCOM dataDifferent Contaminants - Slush

    Slush:

    2 mm: wet> 2 mm: contaminated

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    FCOM dataDifferent Contaminants - Wet snow

    Wet snow:

    4 mm: wet> 4 mm: contaminated

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    FCOM dataDifferent Contaminants - Dry snow

    Dry snow:

    15 mm: wet> 15 mm: contaminated

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    18Performance on contaminated runways - Friction coefficient - Crosswind - Use of FCOM

    WET or CONTAMINATED?

    15 mm: wet

    4 mm: wet 2 mm: wet 3 mm: wet

    Dry SnowWet SnowSlushStanding Water

    FCOM dataDifferent Contaminants - Summary

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    In case of a wet

    runway use:

    WET runway corrections

    FCOM data

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    In case of a contami-

    nated runway: Standing Water > 3 mm:

    depth 3 mm ~ 6.3 mm

    depth 6.3 mm ~ 12.7 mm

    Slush > 2 mm:

    depth 2 mm ~ 6.3 mm

    depth 6.3 mm ~ 12.7 mm

    FCOM data

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    21Performance on contaminated runways - Friction coefficient - Crosswind - Use of FCOM

    In case of a contaminated runway:

    Wet Snow > 4 mm:

    12.7 mm (1/2 inch) wet snow isequivalent to 6.3 mm (1/4 inch)

    slush.

    Dry Snow > 15 mm:50.8 mm (2 inches) dry snow is

    equivalent to 6.3 mm (1/4 inch)

    slush.

    Compacted Snow:

    12.7 mm6.3 mm=

    Wet Snow Slush

    50.8 mm

    6.3 mm=

    Dry Snow Slush

    FCOM data

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    15 mm

    4 mm2 mm3 mm

    Dry SnowWet SnowSlushStanding Water

    any depth

    Compacted Snow

    12.7 mm 12.7 mm

    25.4 mm

    6.3 mm 6.3 mm

    12.7 mm

    50.8 mm

    Wet runway corrections

    15 mm

    4 mm2 mm3 mm

    FCOM data - Summary

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    Dry SnowWet SnowSlushStanding Water

    any depth

    Compacted Snow

    12.7 mm

    25.4 mm

    6.3 mm

    12.7 mm

    50.8 mm

    15 mm

    4 mm2 mm3 mm

    Contaminated

    runway corrections

    12.7 mm

    6.3 mm

    FCOM data - Summary

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    Dry SnowWet SnowSlushStanding Water

    any depth

    Compacted Snow

    12.7 mm 12.7 mm

    25.4 mm

    6.3 mm

    15 mm

    4 mm2 mm3 mm

    Contaminated

    runway corrections

    6.3 mm

    12.7 mm

    50.8 mm

    FCOM data - Summary

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    Dry SnowWet SnowSlushStanding Water

    any depth

    Compacted Snow

    12.7 mm

    6.3 mm 6.3 mm

    12.7 mm

    50.8 mm

    15 mm

    4 mm2 mm3 mm

    12.7 mm

    25.4 mm

    Contaminatedrunway corrections

    FCOM data - Summary

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    Dry SnowWet SnowSlushStanding Water Compacted Snow

    12.7 mm 12.7 mm

    25.4 mm

    6.3 mm 6.3 mm

    12.7 mm

    50.8 mm

    15 mm

    4 mm2 mm3 mm

    Contaminatedrunway corrections

    any depth

    FCOM data - Summary

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    Dry SnowWet SnowSlushStanding Water

    any depth

    Compacted Snow

    12.7 mm 12.7 mm

    25.4 mm

    6.3 mm 6.3 mm

    12.7 mm

    50.8 mm

    15 mm

    4 mm2 mm3 mm

    FCOM data - Summary

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    28Performance on contaminated runways - Friction coefficient - Crosswind - Use of FCOM

    Performance determination Landing: refer to FCOM tables

    Takeoff: Different methods are available depending on each

    airlines

    The level of conservatism or details and difficulty

    depends on the method

    Takeoff chart DRY + FCOM correction

    Takeoff chart DRY + takeoff chart correction(OCTOPUS: A319, A321, A330, A340)

    Takeoff chart CONTAMINATED

    Less Paper Cockpit program (LPC)

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    29Performance on contaminated runways - Friction coefficient - Crosswind - Use of FCOM

    FCOM:

    Landing distances

    Performance determination - Landing

    For all runway conditions

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    Takeoff chart DRY + FCOM correction

    - Takeoff chart DRY

    Performance determination - Takeoff

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    Performance determination - TakeoffTakeoff chart DRY + FCOM correction

    - FCOM corrections

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    Performance determination - Takeoff Takeoff chart DRY + Takeoff chart correction

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    Performance determination - Takeoff Takeoff chart CONTAMINATED

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    Performance determination - Takeoff Less Paper Cockpit (LPC) program

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    Airport : Airbus City, runway 31

    OAT = 5oC, No wind, Standard QNH

    Runway covered with 5 mm slush

    Performance determination - TakeoffExample: A330-223

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    245.9 3/6

    159/62/67

    Performance determination - TakeoffTakeoff chart DRY + FCOM correction

    - Takeoff chart DRY

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    Takeoff chart DRY +

    FCOM correction- FCOM corrections

    Performance determination - Takeoff

    24.8

    MTOW DRY 245.9Correction - 24.8

    Corrected Weight 221.1

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    Performance determination - Takeoff

    MTOW DRY 245.9

    Correction - 24.8Corrected Weight 221.1

    Takeoff chart DRY +

    FCOM correction- FCOM corrections

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    Takeoff chart DRY+ Takeoff chart

    correction

    Performance determination - Takeoff245.9 3/6

    159/62/67

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    Performance determination - Takeoff

    MTOWDRY

    245.9

    Correction - 23.2

    MTOW1/4 SLUSH

    222.7

    Takeoff chart DRY+ Takeoff chart

    correction

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    225.0 3/3

    142/52/55

    Performance determination - TakeoffTakeoff chart CONTAMINATED (Slush 1/4)

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    Performance determination - Takeoff Less Paper Cockpit (LPC) program

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    Performance determination - Takeoff Less Paper Cockpit (LPC) program

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    Performance determination - Takeoff Less Paper Cockpit (LPC) program

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    A330-223

    Airport : Airbus City, runway 31

    OAT = 5oC, No wind, Standard QNH

    Runway covered with 5 mm slush

    Performance determination - Takeoff

    Takeoff chart

    DRY + FCOM

    correction

    Takeoff chart

    DRY + chart

    correction

    Takeoff chart

    SLUSH(*)

    LPC

    program

    221.1 t 222.7 t 225 t 225 t

    Method

    Takeoff

    weight

    Difficulty

    of use

    Summary

    (*) If max TO weight SLUSH > max TO weight DRY, take max TO weight DRY

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    46Performance on contaminated runways - Friction coefficient - Crosswind - Use of FCOM

    CrosswindDemonstrated crosswind

    A demonstrated crosswind is given in the FCOM Demonstrated : Maximum crosswind which was

    experienced during the flight test campaign.

    Applicable fordry and wet runways.

    Demonstrated crosswind is not a limitation.

    This is an information providing an indication of what

    was experienced during flight test to give some

    guidance for operators to establish their own

    limitations.

    FAR/JAR 25 requires this information to be given.

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    Crosswind

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    Crosswind on contaminated runways

    A poor runway friction coefficient affects both

    braking actionanddirectional control and thus

    the capability to sustain high crosswinds fortakeoff and landing

    Airbus has issued some recommendations based

    on calculation and operational experience

    Crosswind

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    CrosswindCrosswind on

    contaminatedrunways

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    Conclusion On wet and contaminated runways it is mandatory

    to get the type and depth of contaminant Reported runway friction coefficient (Mu) and estimated

    braking action are of no use to determine takeoff and

    landing performance

    Several tools and methods exist to determinetakeoff performance

    When operating regularly on contaminated

    runways it is recommended to publish takeoff

    charts for the associated contaminant